CA994891A - Solar torque compensation for a satellite - Google Patents
Solar torque compensation for a satelliteInfo
- Publication number
- CA994891A CA994891A CA164,488A CA164488A CA994891A CA 994891 A CA994891 A CA 994891A CA 164488 A CA164488 A CA 164488A CA 994891 A CA994891 A CA 994891A
- Authority
- CA
- Canada
- Prior art keywords
- satellite
- torque compensation
- solar torque
- solar
- compensation
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
- B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
- B64G1/32—Guiding or controlling apparatus, e.g. for attitude control using earth's magnetic field
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
- B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
- B64G1/283—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect using reaction wheels
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
- B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
- B64G1/361—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors using star sensors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
- B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
- B64G1/363—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors using sun sensors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
- B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
- B64G1/365—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors using horizon or Earth sensors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
- B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
- B64G1/369—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors using gyroscopes as attitude sensors
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S136/00—Batteries: thermoelectric and photoelectric
- Y10S136/291—Applications
- Y10S136/292—Space - satellite
Landscapes
- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Radar, Positioning & Navigation (AREA)
- Aviation & Aerospace Engineering (AREA)
- General Life Sciences & Earth Sciences (AREA)
- Geochemistry & Mineralogy (AREA)
- Geology (AREA)
- Environmental & Geological Engineering (AREA)
- Life Sciences & Earth Sciences (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Electric Propulsion And Braking For Vehicles (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1293572A GB1413658A (en) | 1972-03-20 | 1972-03-20 | Solar torque compensation for a satellite or other spacecraft |
Publications (1)
Publication Number | Publication Date |
---|---|
CA994891A true CA994891A (en) | 1976-08-10 |
Family
ID=10013846
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA164,488A Expired CA994891A (en) | 1972-03-20 | 1973-02-23 | Solar torque compensation for a satellite |
Country Status (6)
Country | Link |
---|---|
US (1) | US3838834A (en) |
JP (1) | JPS496700A (en) |
CA (1) | CA994891A (en) |
DE (1) | DE2313606A1 (en) |
FR (1) | FR2177364A5 (en) |
GB (1) | GB1413658A (en) |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS50152500A (en) * | 1974-05-30 | 1975-12-08 | ||
US4009851A (en) * | 1974-12-23 | 1977-03-01 | Rca Corporation | Spacecraft structure |
FR2544919A1 (en) * | 1983-04-21 | 1984-10-26 | Comte Pierre | Guidance of large-size satellites with low density by electromagnetic effect |
FR2615477B1 (en) * | 1987-05-22 | 1989-08-18 | Centre Nat Etd Spatiales | DEVICE AND METHOD FOR POINTING A SPATIAL PROBE TOWARDS A CELESTIAL BODY |
FR2665418B1 (en) * | 1990-07-31 | 1995-05-24 | Aerospatiale | ARTIFICIAL SATELLITE STABILIZED IN ATTITUDE BY PASSIVE COMPENSATION OF SOLAR RADIATION PRESSURE. |
US5413293A (en) * | 1992-12-22 | 1995-05-09 | Hughes Aircraft Company | Magnetic torque attitude control systems |
US6089509A (en) * | 1997-04-01 | 2000-07-18 | Motorola, Inc. | Spacecraft attitude control using electrical power subsystem |
RU2474519C2 (en) * | 2011-04-26 | 2013-02-10 | Федеральное Государственное Образовательное Учреждение Высшего Профессионального Образования "Саратовский Государственный Аграрный Университет Имени Н.И. Вавилова" | Device to turn aircraft |
CN102431659B (en) * | 2011-10-27 | 2013-07-24 | 北京航空航天大学 | Halo orbit detector structure of sun-earth system and attitude directing thereof |
US10618678B1 (en) * | 2015-10-20 | 2020-04-14 | Space Systems/Loral, Llc | Self-balancing solar array |
CN106275510B (en) * | 2016-08-26 | 2018-07-24 | 北京控制工程研究所 | A kind of electromechanical integration magnetic torquer structure |
FR3058012B1 (en) * | 2016-10-21 | 2020-01-10 | Airbus Defence And Space Sas | COMBINED LASER SIGNAL IMAGING AND COMMUNICATION SYSTEM |
CN116395148B (en) * | 2023-03-20 | 2023-09-15 | 银河航天(北京)网络技术有限公司 | Satellite and rocket separation control system and control method |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3070699A (en) * | 1961-09-26 | 1962-12-25 | William L Lehmann | Photovoltaic solar orienting device |
US3232561A (en) * | 1963-06-06 | 1966-02-01 | Honeywell Inc | Control apparatus for space craft |
US3326497A (en) * | 1964-07-24 | 1967-06-20 | Hoffman Electronics Corp | Solar cell array |
US3304028A (en) * | 1964-08-11 | 1967-02-14 | Hugh L Dryden | Attitude control for spacecraft |
US3367605A (en) * | 1964-09-16 | 1968-02-06 | Gen Electric | Radiation-operated attitude control |
DE1506140A1 (en) * | 1966-02-01 | 1969-03-27 | Gen Electric | Orientation device for satellites |
US3390848A (en) * | 1966-05-19 | 1968-07-02 | Air Force Usa | Magnetic torquing of spin axis stabilization |
US3588000A (en) * | 1968-07-29 | 1971-06-28 | Westinghouse Electric Corp | Orbit position control of planar reflector satellites |
-
1972
- 1972-03-20 GB GB1293572A patent/GB1413658A/en not_active Expired
- 1972-12-29 US US00319366A patent/US3838834A/en not_active Expired - Lifetime
-
1973
- 1973-02-23 CA CA164,488A patent/CA994891A/en not_active Expired
- 1973-03-19 DE DE2313606A patent/DE2313606A1/en not_active Withdrawn
- 1973-03-20 FR FR7309997A patent/FR2177364A5/fr not_active Expired
- 1973-03-20 JP JP48032522A patent/JPS496700A/ja active Pending
Also Published As
Publication number | Publication date |
---|---|
US3838834A (en) | 1974-10-01 |
JPS496700A (en) | 1974-01-21 |
GB1413658A (en) | 1975-11-12 |
FR2177364A5 (en) | 1973-11-02 |
DE2313606A1 (en) | 1973-09-27 |
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